CN109967850B - Connection method for resistance spot welding of CoCrCuFeNi high-entropy alloy - Google Patents

Connection method for resistance spot welding of CoCrCuFeNi high-entropy alloy Download PDF

Info

Publication number
CN109967850B
CN109967850B CN201910330256.1A CN201910330256A CN109967850B CN 109967850 B CN109967850 B CN 109967850B CN 201910330256 A CN201910330256 A CN 201910330256A CN 109967850 B CN109967850 B CN 109967850B
Authority
CN
China
Prior art keywords
entropy alloy
spot welding
resistance spot
cocrcufeni high
cocrcufeni
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201910330256.1A
Other languages
Chinese (zh)
Other versions
CN109967850A (en
Inventor
秦庆东
李娟�
张英哲
伍玉娇
龙琼
伍剑明
苏向东
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Guizhou Institute of Technology
Original Assignee
Guizhou Institute of Technology
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Guizhou Institute of Technology filed Critical Guizhou Institute of Technology
Priority to CN201910330256.1A priority Critical patent/CN109967850B/en
Publication of CN109967850A publication Critical patent/CN109967850A/en
Application granted granted Critical
Publication of CN109967850B publication Critical patent/CN109967850B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K11/00Resistance welding; Severing by resistance heating
    • B23K11/10Spot welding; Stitch welding
    • B23K11/11Spot welding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K11/00Resistance welding; Severing by resistance heating
    • B23K11/34Preliminary treatment

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Resistance Welding (AREA)

Abstract

The invention discloses a connecting method of resistance spot welding of a CoCrCuFeNi high-entropy alloy. According to the invention, the metal foils of Ti, Cu, Al and Ag are used as the intermediate solder layers, resistance spot welding is carried out on the CoCrCuFeNi high-entropy alloy base material, and the welded CoCrCuFeNi high-entropy alloy has high shear strength.

Description

Connection method for resistance spot welding of CoCrCuFeNi high-entropy alloy
Technical Field
The invention relates to a connecting method for resistance spot welding, in particular to a connecting method capable of realizing resistance spot welding of a CoCrCuFeNi high-entropy alloy.
Background
The high-entropy alloy becomes a special alloy system due to the microstructure of the full solid solution phase, and is characterized in that the high-entropy alloy breaks through the design concept that the traditional alloy material is mainly made of a certain alloy element, is prepared by five or more elements with equal atoms, and forms a multi-principal-element alloy system. The multi-principal element system is an alloy system which forms higher mixed entropy and configuration entropy and forms a full solid solution microstructure under the drive of high entropy, so the multi-principal element system is also called as high-entropy alloy. Due to the existence of the full solid solution structure, no brittle metal piece compound is formed, and the integral structure is face-centered cubic or body-centered cubic or the mixture of the face-centered cubic and the body-centered cubic. The special structure leads to the formation of special mechanical properties and physical properties. Therefore, different types of high-entropy alloys show different excellent properties, such as strength, hardness, wear resistance, corrosion resistance, thermal resistance, electric resistance, magnetic properties and the like. Although much research work has been carried out on high-entropy alloys, welding is a common connection mode for engineering application as a structural material application, especially large-scale industrial application and equipment manufacturing, and at present, research work carried out on the aspect of welding of high-entropy alloys is less, and related documents which can be retrieved can be circled. The CoCrCuFeNi serving as the earliest researched high-entropy alloy system has excellent toughness, good strength and wide application prospect. Therefore, the research and development of a connection method aiming at the resistance spot welding of the CoCrCuFeNi high-entropy alloy is a technical problem to be solved urgently.
Disclosure of Invention
The invention aims to provide a connection method for resistance spot welding of a CoCrCuFeNi high-entropy alloy. The method can ensure that the CoCrCuFeNi high-entropy alloy can be effectively connected by a resistance electric welding method in the engineering application process.
The technical scheme of the invention is as follows: a connection method for resistance spot welding of CoCrCuFeNi high-entropy alloy is characterized in that after CoCrCuFeNi high-entropy alloy base metals to be welded are polished and cleaned, metal foils of Ti, Cu, Al and Ag are filled among the base metals to serve as an intermediate layer, and welding is completed after direct-current resistance spot welding.
In the connection method for resistance spot welding of the CoCrCuFeNi high-entropy alloy, the CoCrCuFeNi high-entropy alloy base material to be welded is polished by sand paper, then is cleaned by ultrasonic for 30 minutes and then is dried.
In the connection method of resistance spot welding of the CoCrCuFeNi high-entropy alloy, the Ti, Cu, Al and Ag metal foils are consistent in thickness and 5-30 mu m in thickness, and are polished by sand paper, cleaned by ultrasonic for 30 minutes and dried.
In the foregoing connection method for resistance spot welding of the CoCrCuFeNi high-entropy alloy, the stacking order of the Ti, Cu, Al, and Ag metal foils is: Ti/Cu/Al/Ag, or Ti/Al/Cu/Ag, or Ti/Cu/Ag/Al, or Ti/Ag/Cu/Al.
In the connection method of resistance spot welding of the CoCrCuFeNi high-entropy alloy, the welding current of resistance spot welding is 1-40kA, and the welding time is 100-1000 ms.
The invention has the beneficial effects that: compared with the prior art, the invention uses Ti, Cu, Al and Ag metal foils as intermediate solder layers to perform resistance spot welding on the CoCrCuFeNi high-entropy alloy base material, and the welded CoCrCuFeNi high-entropy alloy has higher shear strength. The applicant tests the shear strength values of the CoCrCuFeNi high-entropy alloys welded in the examples 1, 2 and 3 respectively, each group is tested 10 times, the test results are averaged, and the test results are recorded, which is shown in Table 1.
Table 1 results of performance testing
Figure BDA0002037463720000021
As can be seen from the table, the mechanical properties of the CoCrCuFeNi high-entropy alloy welded according to examples 1, 2 and 3 reach 0.6 times of the ultimate tensile strength of the parent metal, and therefore, considerable mechanical properties are obtained after the resistance spot welding connection of the invention.
Detailed Description
The present invention is further illustrated by the following examples, which are not to be construed as limiting the invention.
Example 1 of the invention:
two pieces of CoCrCuFeNi high-entropy alloy with the size of 150 multiplied by 100 multiplied by 10 mm are connected by resistance spot welding.
And (3) polishing the surface of the CoCrCuFeNi high-entropy alloy parent metal by using sand paper, cleaning for 30 minutes by using ultrasonic waves, and drying. And (2) polishing Ti, Cu, Al and Ag foils with the thickness of 5 mu m by using sand paper, ultrasonically cleaning for 30 minutes, drying, clamping between two CoCrCuFeNi high-entropy alloy base metals to be welded according to the stacking sequence of Ti/Cu/Al/Ag, placing between electrodes of resistance spot welding, setting the current to be 1kA and the welding time to be 100ms, and cooling to finish welding.
Example 2 of the invention:
two pieces of CoCrCuFeNi high-entropy alloy with the size of 180 multiplied by 100 multiplied by 15 mm are connected by resistance spot welding.
And (3) polishing the surface of the CoCrCuFeNi high-entropy alloy parent metal by using sand paper, cleaning for 30 minutes by using ultrasonic waves, and drying. Polishing Ti, Cu, Al and Ag foils with the thickness of 10 mu m by using sand paper, ultrasonically cleaning for 30 minutes, drying, clamping between two CoCrCuFeNi high-entropy alloy base metals to be welded according to the stacking sequence of Ti/Al/Cu/Ag, placing between electrodes of resistance spot welding, setting the current to be 10kA and the welding time to be 300ms, and cooling to finish welding.
Example 3 of the invention:
two pieces of CoCrCuFeNi high-entropy alloy with the size of 180 multiplied by 100 multiplied by 25 mm are connected by resistance spot welding.
And (3) polishing the surface of the CoCrCuFeNi high-entropy alloy parent metal by using sand paper, cleaning for 30 minutes by using ultrasonic waves, and drying. And (2) polishing Ti, Cu, Al and Ag foils with the thickness of 20 mu m by using sand paper, ultrasonically cleaning for 30 minutes, drying, clamping between two CoCrCuFeNi high-entropy alloy base metals to be welded according to the stacking sequence of Ti/Cu/Ag/Al, placing between electrodes of resistance spot welding, setting the current to be 20kA and the welding time to be 500ms, and cooling to finish welding.
Example 4 of the invention:
two pieces of CoCrCuFeNi high-entropy alloy with the size of 180 multiplied by 100 multiplied by 35 mm are connected by resistance spot welding.
And (3) polishing the surface of the CoCrCuFeNi high-entropy alloy parent metal by using sand paper, cleaning for 30 minutes by using ultrasonic waves, and drying. Polishing Ti, Cu, Al and Ag foils with the thickness of 25 mu m by using sand paper, ultrasonically cleaning for 30 minutes, drying, clamping between two base materials to be welded according to the stacking sequence of Ti/Ag/Cu/Al, placing between electrodes for resistance welding, setting the current to be 40kA and the welding time to be 1000ms, and cooling to finish welding. Mechanical property test experiments show that the shear strength after welding reaches 252 MPa.
Example 5 of the invention:
two pieces of CoCrCuFeNi high-entropy alloy with the size of 180 multiplied by 100 multiplied by 8 mm are connected by resistance spot welding.
And (3) polishing the surface of the CoCrCuFeNi high-entropy alloy parent metal by using sand paper, cleaning for 30 minutes by using ultrasonic waves, and drying. Polishing Ti, Cu, Al and Ag foils with the thickness of 8 mu m by using sand paper, ultrasonically cleaning for 30 minutes, drying, clamping between two CoCrCuFeNi high-entropy alloy base metals to be welded according to the stacking sequence of Ti/Ag/Cu/Al, placing between electrodes of resistance spot welding, setting the current to be 18kA and the welding time to be 600ms, and cooling to finish welding. The mechanical property test experiment shows that the shear strength after welding reaches 250 MPa.

Claims (5)

1. A connection method of resistance spot welding of CoCrCuFeNi high-entropy alloy is characterized in that: after polishing and cleaning CoCrCuFeNi high-entropy alloy base metals to be welded, filling Ti, Cu, Al and Ag metal foils between the base metals as an intermediate layer, and completing welding after direct-current resistance spot welding.
2. The method for connecting the CoCrCuFeNi high-entropy alloy by resistance spot welding according to claim 1, is characterized in that: and polishing the CoCrCuFeNi high-entropy alloy base metal to be welded by using sand paper, then ultrasonically cleaning for 30 minutes, and then drying.
3. The method for connecting the CoCrCuFeNi high-entropy alloy by resistance spot welding according to claim 1, is characterized in that: the Ti, Cu, Al and Ag metal foils are consistent in thickness and 5-30 mu m in thickness, and are polished by abrasive paper, cleaned by ultrasonic for 30 minutes and dried.
4. The method for connecting the CoCrCuFeNi high-entropy alloy by resistance spot welding according to claim 1, is characterized in that: the stacking sequence of the Ti, Cu, Al and Ag metal foils is as follows: Ti/Cu/Al/Ag, or Ti/Al/Cu/Ag, or Ti/Cu/Ag/Al, or Ti/Ag/Cu/Al.
5. The method for connecting the CoCrCuFeNi high-entropy alloy by resistance spot welding according to claim 1, is characterized in that: the welding current of resistance spot welding is 1-40kA, and the welding time is 100-1000 ms.
CN201910330256.1A 2019-04-23 2019-04-23 Connection method for resistance spot welding of CoCrCuFeNi high-entropy alloy Active CN109967850B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910330256.1A CN109967850B (en) 2019-04-23 2019-04-23 Connection method for resistance spot welding of CoCrCuFeNi high-entropy alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910330256.1A CN109967850B (en) 2019-04-23 2019-04-23 Connection method for resistance spot welding of CoCrCuFeNi high-entropy alloy

Publications (2)

Publication Number Publication Date
CN109967850A CN109967850A (en) 2019-07-05
CN109967850B true CN109967850B (en) 2021-02-05

Family

ID=67085953

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910330256.1A Active CN109967850B (en) 2019-04-23 2019-04-23 Connection method for resistance spot welding of CoCrCuFeNi high-entropy alloy

Country Status (1)

Country Link
CN (1) CN109967850B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11339817B2 (en) 2016-08-04 2022-05-24 Honda Motor Co., Ltd. Multi-material component and methods of making thereof
US11318566B2 (en) 2016-08-04 2022-05-03 Honda Motor Co., Ltd. Multi-material component and methods of making thereof
US11511375B2 (en) 2020-02-24 2022-11-29 Honda Motor Co., Ltd. Multi component solid solution high-entropy alloys

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101590574B (en) * 2009-06-29 2011-09-28 西安理工大学 High-entropy alloy brazing filler metal for welding TA2 and 0Cr18Ni9Ti and preparation method thereof
CN103252568B (en) * 2013-04-23 2016-01-20 上海工程技术大学 A kind of for filling spot welding stainless steel high-entropy alloy powder and the stainless process of a kind of high-entropy alloy powder filling spot welding
US10668566B2 (en) * 2016-01-27 2020-06-02 H.C. Starck Inc. Fabrication of high-entropy alloy wire and multi-principal element alloy wire
US10640854B2 (en) * 2016-08-04 2020-05-05 Honda Motor Co., Ltd. Multi-material component and methods of making thereof
CN108747006B (en) * 2018-06-12 2020-07-14 贵州理工学院 Laser welding method of CoCrCuFeNi high-entropy alloy

Also Published As

Publication number Publication date
CN109967850A (en) 2019-07-05

Similar Documents

Publication Publication Date Title
CN109967850B (en) Connection method for resistance spot welding of CoCrCuFeNi high-entropy alloy
CN109967852B (en) Diffusion welding connection method for CoCrCuFeNi high-entropy alloy
CN109909643B (en) Medium-entropy alloy material for welding and welding method
CN101254572B (en) Method for diffusion welding titanium alloy and copper alloy using niobium central layer
US10115655B2 (en) Heat dissipation substrate and method for producing heat dissipation substrate
Ting et al. Influences of different filler metals on electron beam welding of titanium alloy to stainless steel
CN102059449B (en) Diffusion welding method of tungsten alloy and tantalum alloy at low temperature
CN102218592A (en) Diffusion welding method of titanium or titanium alloy and stainless steel
CN110405300B (en) Method for preparing high-strength AlCoCrFeNi high-entropy alloy joint by adopting Ni-based brazing filler metal
CN113399861B (en) Copper-nickel-based welding wire for copper-steel transition layer melting-brazing and preparation method thereof
CN109967812B (en) Brazing connection method of CoCrCuFeNi high-entropy alloy
CN107414279B (en) A kind of connection method for slab TiNi alloy and titanium alloy dissimilar materials
CN104014922A (en) Fast-diffusion welding method of hard alloy and steel
CN102218594A (en) Low-temperature diffusion welding method for molybdenum alloy and copper alloy
CN106181000A (en) A kind of tungsten alloy and the method for attachment of molybdenum alloy
CN113732467B (en) Composite intermediate layer for tungsten/steel connecting piece and diffusion welding method
CN111318778B (en) Stepwise brazing method for toughening titanium alloy and high-temperature alloy brazed joint
CN109971988B (en) Ultrahigh-strength copper-titanium alloy and preparation method thereof
CN110900037B (en) Brazing filler metal and method for welding molybdenum-rhenium alloy and steel
Narendranath et al. Effect of FSW on microstructure and hardness of AA6061/SiC/fly ash MMCs
CN113774374A (en) Steel-based titanium coating and preparation method and application thereof
CN113399860A (en) Nickel-based welding wire for copper-steel composite plate transition layer and preparation method thereof
CN111331280B (en) High-entropy alloy preform and TA2/0Cr18Ni9 fusion welding method
CN111687530B (en) Method for compounding hydrogen absorption expansion substance and other materials
JP6333268B2 (en) Layer composite

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant